EN 2209:2008
(Main)Aerospace series - Steel FE-PL1502 (25CrMo4) - 900 MPa ≤ Rm ≤ 1 100 MPa - Sheets, strips and plates - 0,5 mm ≤ a ≤ 20 mm
Aerospace series - Steel FE-PL1502 (25CrMo4) - 900 MPa ≤ Rm ≤ 1 100 MPa - Sheets, strips and plates - 0,5 mm ≤ a ≤ 20 mm
This standard specifies the requirements relating to:
Steel FE-PL1502 (25CrMo4)
900 MPa ≤ Rm ≤ 1 100 MPa
Sheets, strips and plates
0,5 mm ≤ a ≤ 20 mm
for aerospace applications.
Luft- und Raumfahrt - Stahl FE-PL1502 (25CrMo4) - 900 MPa ≤ Rm ≤ 1 100 MPa - Bleche, Bänder und Platten - 0,5 mm ≤ a ≤ 20 mm
Diese Norm legt die Anforderungen an
Stahl FE-PL1502 (25CrMo4)
900 MPa ≤ Rm ≤ 1 100 MPa
Bleche, Bänder und Platten
0,5 mm ≤ a ≤ 20 mm
für Anwendungen in der Luft- und Raumfahrt fest.
Série aérospatiale - Acier FE-PL1502 (25CrMo4) - 900 MPa ≤ Rm ≤ 1 100 MPa - Tôles, bandes et plaques - 0,5 mm ≤ a ≤ 20 mm
Aeronavtika - Jeklo FE-PL1502 (25CrMo4) - 900 MPa ≤ Rm ≤ 1 100 MPa - Pločevine, trakovi in plošče - 0,5 mm ≤ a ≤ 20 mm
General Information
- Status
- Published
- Publication Date
- 25-Nov-2008
- Withdrawal Date
- 30-May-2009
- Technical Committee
- ASD-STAN - Aerospace
- Drafting Committee
- ASD-STAN/D 4 - Metallic
- Current Stage
- 9093 - Decision to confirm - Review Enquiry
- Start Date
- 21-Jan-2024
- Completion Date
- 21-Jan-2026
Relations
- Effective Date
- 28-Jan-2026
- Effective Date
- 28-Jan-2026
- Effective Date
- 28-Jan-2026
- Effective Date
- 28-Jan-2026
Overview
EN 2209:2008 is a European standard developed by CEN that defines the specifications for Steel FE-PL1502 (25CrMo4), a high-strength alloy tailored for aerospace applications. This standard covers steel sheets, strips, and plates with thicknesses ranging from 0.5 mm to 20 mm and tensile strength between 900 MPa and 1,100 MPa. Specifically designed for the aerospace industry, it ensures materials meet rigorous mechanical and chemical property requirements to support structural integrity, safety, and performance.
Key Topics
Material Specification
EN 2209 covers steel designated FE-PL1502 (25CrMo4), specifying chemical composition limits that include carbon (C), silicon (Si), manganese (Mn), chromium (Cr), molybdenum (Mo), and other alloying elements essential for strength and durability.Mechanical Properties
- Tensile strength (Rm): 900 MPa ≤ Rm ≤ 1,100 MPa
- Proof stress (Rp0.2): minimum values depending on thickness
- Elongation and hardness requirements to assure ductility and wear resistance
- Impact strength values ensure toughness at ambient temperature for thicknesses ≥ 10 mm
Forms and Dimensions
Material is supplied in forms including sheets, strips, and plates with thicknesses from 0.5 mm up to 20 mm, suitable for a variety of aerospace structural components.Heat Treatment and Delivery Conditions
- Annealed, normalized and tempered, or hardened and tempered conditions
- Typical heat treatment includes quenching at 850–880 °C followed by tempering at or above 520 °C
- Delivery condition codes (A, B, U) correspond to specific heat treatment states
Testing and Inspection
- Mechanical testing references per EN 4700-1
- Dimensional and marking inspections ensure compliance with aerospace quality standards
- Qualification procedures align with EN 9133 to standardize aerospace part reliability
Applications
EN 2209:2008 steel is primarily utilized in the aerospace industry where high strength-to-weight ratios and material reliability are crucial. Practical applications include:
- Aircraft structural components such as frames, reinforcements, and brackets
- Engine parts exposed to high mechanical stresses
- Landing gear and support assemblies requiring toughness and fatigue resistance
- Aerospace manufacturing requiring weldable, high-performance steel sheets and plates
This steel grade offers a balance between mechanical strength and processability, making it ideal for critical aerospace parts that demand consistent performance under extreme conditions.
Related Standards
EN 2209:2008 is part of a comprehensive framework of aerospace metallic material standards, including:
- EN 4258: General organization and standardization principles for aerospace metallic materials
- EN 4500-5: Rules for drafting and presenting aerospace material standards, specifically steels
- EN 4700-1: Technical specification for steel and heat-resisting alloys in wrought form (plates, sheets, strips)
- EN 9133: Quality management and qualification procedures for aerospace standard parts
Following these interconnected standards ensures cohesive quality, uniformity, and regulatory compliance in aerospace material selection and use.
Keywords: EN 2209:2008, aerospace steel standard, FE-PL1502, 25CrMo4, high-strength steel sheets, aerospace plates, 900 MPa tensile strength, steel strips aerospace, CEN aerospace standards, aerospace material specifications, aircraft steel sheets
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Frequently Asked Questions
EN 2209:2008 is a standard published by the European Committee for Standardization (CEN). Its full title is "Aerospace series - Steel FE-PL1502 (25CrMo4) - 900 MPa ≤ Rm ≤ 1 100 MPa - Sheets, strips and plates - 0,5 mm ≤ a ≤ 20 mm". This standard covers: This standard specifies the requirements relating to: Steel FE-PL1502 (25CrMo4) 900 MPa ≤ Rm ≤ 1 100 MPa Sheets, strips and plates 0,5 mm ≤ a ≤ 20 mm for aerospace applications.
This standard specifies the requirements relating to: Steel FE-PL1502 (25CrMo4) 900 MPa ≤ Rm ≤ 1 100 MPa Sheets, strips and plates 0,5 mm ≤ a ≤ 20 mm for aerospace applications.
EN 2209:2008 is classified under the following ICS (International Classification for Standards) categories: 49.025.10 - Steels. The ICS classification helps identify the subject area and facilitates finding related standards.
EN 2209:2008 has the following relationships with other standards: It is inter standard links to EN 9133:2018, EN 4258:2024, EN 4700-002:2025, EN ISO 2810:2004. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.
EN 2209:2008 is available in PDF format for immediate download after purchase. The document can be added to your cart and obtained through the secure checkout process. Digital delivery ensures instant access to the complete standard document.
Standards Content (Sample)
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.49.025.10JeklaSteelsICS:Ta slovenski standard je istoveten z:EN 2209:2008SIST EN 2209:2009en01-januar-2009SIST EN 2209:2009SLOVENSKI
STANDARD
EUROPEAN STANDARD NORME EUROPÉENNE EUROPÄISCHE NORM
EN 2209
November 2008 ICS 49.025.10 English Version
Aerospace series - Steel FE-PL1502 (25CrMo4) - 900 MPa ≤ Rm ≤ 1 100 MPa - Sheets, strips and plates - 0,5 mm ≤ a ≤ 20 mm
Série aérospatiale - Acier FE-PL1502 (25CrMo4) -900 MPa ≤ Rm ≤ 1 100 MPa - Tôles, bandes et plaques - 0,5 mm ≤ a ≤ 20 mm
Luft- und Raumfahrt - Stahl FE-PL1502 (25CrMo4) - 900 MPa ≤ Rm ≤ 1 100 MPa - Bleche, Bänder und Platten -0,5 mm ≤ a ≤ 20 mm This European Standard was approved by CEN on 16 August 2008.
CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this European Standard the status of a national standard without any alteration. Up-to-date lists and bibliographical references concerning such national standards may be obtained on application to the CEN Management Centre or to any CEN member.
This European Standard exists in three official versions (English, French, German). A version in any other language made by translation under the responsibility of a CEN member into its own language and notified to the CEN Management Centre has the same status as the official versions.
CEN members are the national standards bodies of Austria, Belgium, Bulgaria, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and United Kingdom.
EUROPEAN COMMITTEE FOR STANDARDIZATION
COMITÉ EUROPÉEN DE NORMALISATION EUROPÄISCHES KOMITEE FÜR NORMUNG
Management Centre: rue de Stassart, 36
B-1050 Brussels © 2008 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 2209:2008: ESIST EN 2209:2009
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